Apparatus and method for eliminating varying pressure fluctuations in a pressure transducer

ABSTRACT

A single pressure sensing capsule has a reference pressure ported to the rear side of a silicon sensing die. The front side of the silicon sensing die receives a main pressure at another port. The silicon sensing die contains a full Wheatstone bridge on one of the surfaces and within the active area designated as the diaphragm area. Thus, the difference of the main and reference pressure results in the sensor providing an output equivalent to the differential pressure, namely the main pressure minus the reference pressure which is the stress induced in a sensing diaphragm. In any event, the reference pressure or main pressure may be derived from a pump pressure which is being monitored. The pump pressure output is subjected to a pump ripple or a sinusoidally varying pressure. In order to compensate for pump ripple, one employs a coiled tube. The tube length is selected to suppress the pump ripple as applied to the sensor die. In this manner, the pump ripple cannot cause resonance which would result in pressure amplification and which pressure amplification would destroy the sensor.

RELATED APPLICATIONS

This application is a continuation application claiming priority under 35 U.S.C. §120 to U.S. patent application Ser. No. 12/151,816, filed on 9 May 2008, entitled “APPARATUS AND METHOD FOR ELIMINATING VARYING PRESSURE FLUCTUATIONS IN A PRESSURE TRANSDUCER”, which is hereby incorporated in its entirety as if fully set forth herein.

FIELD OF THE INVENTION

This invention relates to pressure transducers and more particularly to a differential pressure transducer employing a coiled tube to eliminate varying pressure fluctuations.

BACKGROUND OF THE INVENTION

Differential pressure measuring devices usually include one of two design variations. In a first design two half bridge circuits are connected together to form a Wheatstone bridge. The half bridges are normally provided on a silicon sensing die. In this case, there are two separate dies, with a half bridge on each. Each of the devices are ported to the main or reference pressure. One device is ported to the reference pressure. For a differential pressure measurement, the half bridges are electrically connected to electrically subtract the high or main pressure from the low or reference pressure resulting in a voltage proportional to the difference pressure. These techniques are well known. See for example U.S. Pat. No. 6,612,179 issued on Sep. 2, 2003 to A. D. Kurtz and assigned to the assignee herein, namely Kulite Semiconductor Products and entitled Method and Apparatus for the Determination of Absolute Pressure and Differential Pressure Therefrom. This patent describes the combination of absolute and differential pressure sensing devices including a plurality of absolute pressure transducers, each transducer including a plurality of half bridge piezoresistive structures and a device which selectively couples at least one of the half bridges to another half bridge.

In other prior art configurations, a single pressure sensing capsule is employed with the reference pressure ported to the rear side of the silicon sensing die. The main pressure is ported to the top side of the silicon sensing die. This design requires the use of a Wheatstone bridge on a single die. The difference of the main and reference pressure results in the differential pressure. Again, the differential pressure results in a voltage output. This design requires the reference tube to be connected to the reference pressure inlet. In any event, in actual operation both types of differential pressure measuring devices can be subjected to pump ripple, or a sinusoidally varying pressure fluctuation. Normally pump pressure is desirable to be measured in systems having pumps. For example, in an automobile, the oil that lubricates the engine of a car must be forced at high pressure around channels in the engine. In order to operate, a pump is used, which pump normally is referred to as a gear pump. The rotating cam shaft of the engine normally powers the oil pump, driving a shaft that turns a pair of intermeshing gear wheels inside a close fitting chamber. The oil enters the pump where it is trapped by the wheels. The wheels carry the oil around to the outlet, where the teeth come together as they intermesh. This action squeezes the oil and raises its pressure as it is close to the outlet. The speed of pumping is directly linked to the speed of the engine. In any event, in such a pump, the pressure at the output as well as pressure at the input is normally monitored. The pressures are monitored by a pressure transducer. However, these pressure transducers can be subjected to pump ripple or a sinusoidally varying pressure fluctuation. In an adverse situation, the pipe and cavity of the reference or main side of the sensor can be tuned to the frequency of the pump ripple. By this occurring, one creates a resonance in the tube which results in an amplified pressure being applied to the transducer. This amplified pressure can seriously harm the transducer as will be further explained. It is also known that the pump ripple is a function of the number of gear teeth in the pump and the number of revolutions per minute of the teeth. This, as indicated, can vary as the RPM of the pump can vary, and hence such a tube must be selected to filter the range of frequencies to prevent resonance and amplification in the pump operating RPM range. It is understood that the resonance and amplification of the pump ripple pressure can exceed the rating of the sensing die or pressure capability of the structure. Exceeding the rated pressure imparts excessive stress on the die which experiences brittle failure. Aside from loss of the signal from the sensor, on a filter application, contaminates from the dirty side of the filter can be passed to the clean side, thus further destroying the sensor or equipment downstream. One therefore requires a pressure transducer which will operate to eliminate pump ripple or to eliminate varying pressure fluctuations in a sensor and still enable the sensor to be small and compact.

SUMMARY OF THE INVENTION

A differential pressure transducer having a sensor and for providing an output proportional to the difference between a main pressure P₁ and a reference pressure P₂, wherein one of the pressure inputs contains an undesirable varying pressure fluctuation which fluctuation can undesirably produce excessive stress on said sensor, comprising: said sensor having a deflectable diaphragm, said diaphragm having pressure sensing elements on said diaphragm which elements provide an output proportional to an applied pressure on said diaphragm; a first port communicating with one surface of said diaphragm to provide a first pressure thereto; a second port communicating with the other surface of said diaphragm to provide a second pressure thereto, a coiled tube in series with one of said ports and dimensioned to suppress said varying pressure fluctuation prior to the application of said associated pressure to said diaphragm.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 illustrates a cross-sectional view of a differential transducer and housing having two headers according to the prior art.

FIG. 2 is a cross-sectional view of prior art transducer having one header and operative in a differential mode.

FIG. 3 is a diagrammatic view of a pressure transducer having a pipe and cavity and useful for explaining ripple operation.

FIG. 4 is a cross-sectional view of a pressure sensor employing a coiled tube according to this invention.

FIG. 5 is a schematic diagram of a coiled tube according to this invention.

FIG. 6 is a cross-sectional view of a silicon sensor die used in this invention.

FIG. 7 is a schematic diagram of a Wheatstone bridge such as the type employed with the sensor of FIG. 6.

DETAILED DESCRIPTION OF THE FIGURES

Referring to FIG. 1, there is shown a typical prior art differential pressure transducer. The pressure transducer includes a housing 18. In the housing there is a main pressure header 10 and a reference pressure header 14. Both pressure headers contain piezoresistors sensors which are accommodated on silicon diaphragms. As one can ascertain, there is a main pressure port 16 to which a main pressure is applied and a reference pressure port 15 which a reference pressure is applied. The output of the device is proportional to the difference between the main pressure and the reference pressure. The design of FIG. 1 uses two pressure sensing capsules 10 and 14. Each capsule contains a half of a Wheatstone bridge on an associated silicon sensing die. For a differential pressure measurement, the half bridges are electrically connected to electrically subtract the high pressure from the low pressure. Each header is ported to the respective pressure port. Header 10 is ported to the main pressure port 16 and header 14 is ported to the reference pressure port 15. The half bridges on each of these sensors are electrically connected to electrically subtract the high pressure from the low pressure resulting in a voltage proportional to the difference in pressure.

Referring now to FIG. 2, there is shown a prior art pressure transducer which employs a reference tube and is a differential pressure transducer as indicated above. As seen, the pressure sensor or transducer is contained in a metal housing 20. There is a header 23 in the housing which header contains a single die or a semiconductor sensor 22 which basically is a full Wheatstone bridge. As seen, there is a lock nut 24 which couples the reference tube 21 to one side of the sensor 22. This tube 21 receives the reference pressure. The other side of the sensor is exposed to a main pressure port 28. The reference tube couples the reference pressure at port 27 to the other side of the sensor die to cause the Wheatstone bridge to produce an output which is the difference between the reference port pressure and the main port pressure. Therefore, as shown in FIG. 2, a single pressure sensor capsule is used, namely capsule 23. In this prior art design, a full Wheatstone bridge on a single die is used. The difference of the main and reference pressure results in only the differential pressure inducing stress in the sensing diaphragm.

In any event, as can be seen, FIG. 2 shows a single pressure sensing capsule with the reference pressure ported to the rear side of the silicon sensing die and the main pressure ported to the top side. In this design a full Wheatstone bridge on a single die is used as indicated. The difference of the main and reference pressure results in the differential pressure which induces stress in the sensing diaphragm. Again, the differential pressure results in a voltage output from the Wheatstone bridge. The design shown in FIG. 2 requires a reference tube to be connected to the reference pressure inlet. The low delta-p measurements of this design offers a much greater accuracy and hence is a preferred design for low pressure inputs. As indicated above, both designs can be subjected to pump ripple or a sinusoidally varying pressure fluctuation. In an adverse situation, the pipe and cavity of the reference pressure on one side of the sensor can be tuned to the frequency of this pump ripple if this occurs. If this occurs the pressure increases to a level high enough to break or rupture the diaphragm.

Referring to FIG. 3 there is shown a pipe and cavity model which will be employed to explain how an equation for the resonance frequency of a pipe and cavity was derived. As seen in FIG. 3, there is a pipe 30 which has a diameter (d) and a length (l). The pipe has a pressure input port 31 which interfaces with a cavity 32 having a volume (v). The cavity, as well as the pressure inlet interfaces with a pressure transducer 33. Using standard system dynamic analysis, an equation was derived for the resonant frequency of a pipe and cavity as shown in FIG. 3. The port of the pressure sensor 31 is modeled as a series of pipes representing the orifice and fluid channels, and cavities in front of the sensing capsules. The formula for the resonant frequency F_(n) of the pipe/cavity system is: F _(n)=√(3πr ² c ²/4LV)/2π.

Where

-   -   r=internal radius of pipe     -   C=velocity of sound in the pressure fluid     -   L=length of pipe     -   V=volume of the cavity         Thus, as indicated above, when the pipe and cavity structure of         the passage is tuned to the pump ripple frequency, the pump         ripple pressure is amplified. This resonance and amplification         of the pump ripple pressure can exceed the rating of the sensing         die or pressure capability of the structure. Exceeding the rated         pressure applies excessive stresses on the die, which         experiences brittle failure. Aside, from loss of the signal from         the sensor, on a filter application, contaminates from the dirty         side of the filter can be passed to the clean side, thus         destroying the entire sensor or equipment downstream. For large         tube or pipe diameters, the resonance is proportional to the         radius. As the tube diameter gets smaller, capillary action         takes over. As the tube diameter decreases below 0.040 inch, the         change in resonant frequency diminishes. Thus there is a         diminishing return with decreasing tube diameter. In addition,         manufacturability decreases and the likelihood of trapping         particles in the small diameter tube increases. The trapping of         particles will clog the sensor and will decrease reliability. As         can be seen from the above formula, the resonant or critical         frequency Fn is also inversely proportional to the square root         of the length of the pipe. In many design applications, the         frequency can be suppressed merely by increasing the pipe         length. In any event, by increasing the pipe length, one         therefore increases the size of the sensor as the pipe has to be         accommodated.

Referring to FIG. 4 there is shown a differential sensor using a single silicon die (FIG. 2), which silicon die 41 contains a Wheatstone bridge and where the main pressure from a main pressure port 50 is applied to the top surface of the die, while a reference pressure 51 is applied to the bottom surface of the die. As seen, there is a coil 52 which basically is in series with the reference port inlet 51. The coil 52 is a tubular coil which essentially consists of a tube which is wound about a mandril having a screw type thread. In this manner the coil 52 is substantially decreased in length and now can be positioned inside the sensor. The dimensions of the coil are selected according to the above equation and the length of the coil is much longer than the length of the reference port and tube. Normally the reference port inlet would have to be expended by the length of the reference tube or the reference tube extended by the expanded length of the coil 52. This would of course create a problem in manufacturing a small sensor. Thus coiling of the tube 52 keeps the size minimized to aid compact packaging. Also shown in the Figure is header 42 which essentially encompasses the silicon die. There is shown a terminal port 54 which receives leads from the silicon sensing die or from the Wheatstone bridge on the silicon sensing die and directs the outputs through cable 53. As seen, a pressure would be applied to the main port 50 while the reference pressure would be applied to the inlet port 51. The port 51 would be coupled to a pressure associated with a pressure derived from a pump 60. As indicated above, the pump 60 can be a gear pump or any other pump and would contain pump ripple. The pump ripple, due to the fact that it can occur over a fairly wide range of frequency such as 3000 to 5000 cycles will cause resonance in the reference pressure path including tube 44. This resonance will cause amplification of the pressure which could result in exceeding the rating of the sensing die 41. This resonance and amplification of the pump ripple pressure can cause the sensing die to experience brittle failure and therefore destruction. The coil 52 dimensions are selected based on the equation shown above and is maybe wound as indicated on a mandril or on a threaded screw. Typically the coil will have a diameter in the center of approximately ⅜ of an inch with a tube having an outer diameter of 0.04 inches and an inner diameter of 0.02 inches and a length of two or more inches. These dimensions indicate a coil capable of suppressing pump ripple frequency between 3000 to 4000 Hz. It is of course understood that coiled structures have been used in conjunction with pressure transducers for other applications. For example reference is made to U.S. Pat. No. 7,188,528 issued on Mar. 13, 2007 and entitled Low Pass Filter Semiconductor Structures for use in Transducers for Measuring Low Dynamic Pressures in the Presence of High Static Pressures by A. D. Kurtz, et al, an inventor herein, and assigned to Kulite Semiconductor Products, Inc. That patent shows a long tube which basically acts as a low pass filter and will only pass frequencies which are below 120 Hz. In this manner, the dynamic frequency which is 5000 Hz or greater will not pass through the tube. That patent, as indicated, shows a tube for operating as a low pass filter. It is also noted that the tube is not in any manner inserted into the pressure transducer as the tube will be too long to be conveniently employed. Reference is also made to U.S. Pat. No. 7,107,853 issued on Sep. 19, 2006 to A. D. Kurtz, an inventor herein, and entitled Pressure Transducer for Measuring Low Dynamic Pressures in the Presence of High Static Pressures. This patent is the parent application of the above noted patent, both of which are incorporated herein in their entirety. Thus there has been described a coil transducer which will operate to suppress pump ripple and prevent the pump ripple from being amplified and thus destroying the sensing die of a semiconductor pressure transducer.

FIG. 5 shows a coiled tube 52 having a length (L) of 0.4 inches, a tube diameter (d) of 0.04 inches and a coil diameter (D) of ⅜ inches.

Referring to FIG. 6 there is shown a schematic cross-sectional view of a typical sensor module. The sensor module 60 contains a semiconductor substrate having a thin active area or diaphragm 63 upon which piezoresistors such as 61 and 62 are positioned. Such devices are extremely well known and the prior art is replete with semiconductor dies or semiconductor sensors using piezoresistors as 61 and 62 to form a Wheatstone bridge configuration. While two piezoresistors are shown, it is understood that there are normally 4 piezoresistors. The sensor can be protected by coating it with a layer of silicon dioxide and essentially the pressure P₁ is applied to the top of the sensor active area as shown. The pressure may be transmitted to the sensor by an oil-filled cavity which is positioned above the sensor, as is also well known. In any event, the sensor has the pressure P₁ applied to the top side, which for example, may be the main pressure as applied to port 50 of FIG. 4. In any event, the reference pressure P₂, which for example emanates from the pump 60 of FIG. 4 is applied to the underside of the diaphragm. The Wheatstone bridge or sensor provides an output which is equal to P₁−P₂ which is the differential pressure. As seen in FIG. 6, the device is shown in FIG. 4 as sensor 41. Thus the sensor 41 or sensor 60 of FIG. 6 receives a pressure P₁ on the top side and pressure P₂ on the bottom side. As indicated and shown, pressure P₂ is derived from a gear pump 60 which may exhibit pump ripple, which ripple is suppressed by the coil 52 of FIG. 5 as explained in conjunction with FIG. 4.

As shown in FIG. 7 there is a Wheatstone bridge configuration which is a typical sensor structure. The Wheatstone bridge, for example, has four resistors which can be piezoresistors as resistor 91 and so on. The piezoresistors change resistance according to an applied pressure. As seen there are five leads associated with the bridge. Two are used for biasing the bridge and three for providing an output. These leads as shown in FIG. 4 are directed out from the device via cable 53. Thus as shown above, there is a low pressure differential transducer which operates in conjunction with a coil to suppress pump ripple and therefore enable reliable operation during the presence of such ripple or other disturbing variations. This results in improved operation as compared to prior art devices while enabling one to make a extremely small transducer structure.

It should be apparent to one skilled in the state of the art that there are many alternate embodiments which can be determined or are deemed to be encompassed within the spirit and scope of the claims appended hereto. 

1. A differential pressure transducer for providing an output proportional to a difference between a main pressure P₁ and a reference pressure P₂, the differential pressure transducer comprising: a semiconductor sensor comprising an active diaphragm area operative to deflect according to an applied pressure, the active diaphragm area comprising piezoresistors located thereon, the piezoresistors providing a resistance variation according to the applied pressure on the active diaphragm area; a first port communicating with one surface of the diaphragm via a first channel to provide a first pressure thereto; a second port communicating with another surface of the diaphragm to provide a second pressure thereto; and a coiled tube in series with the second port and dimensioned to suppress a varying pressure fluctuation prior to the application of said second pressure to the diaphragm.
 2. The differential pressure transducer according to claim 1, wherein the second pressure is the reference pressure P₂, and wherein the second pressure is derived from a pump that produces pump ripple.
 3. The differential pressure transducer according to claim 2, wherein the pump ripple is between 3000 Hz to 5000 Hz.
 4. The differential pressure transducer according to claim 2, wherein the coiled tube is dimensioned according to the following formula: F _(n)=√(3πr ² c ²/4LV)/2π Where F_(n)=pump ripple frequency r=internal radius of tube c=velocity of sound in pressure fluid L=length of coil V=volume of cavity.
 5. The differential pressure transducer according to claim 1 wherein a diameter of the coiled tube is between ¼ to ½ inches.
 6. The differential pressure transducer according to claim 1 wherein the piezoresistors are connected to a Wheatstone bridge array.
 7. The differential pressure transducer according to claim 1, wherein the varying pressure fluctuation varies sinusoidally.
 8. A method for preventing a sinusoidally varying pressure fluctuation from being amplified in a differential pressure transducer of a type employing a single pressure sensor capsule, the method comprising: applying a main pressure to a front side of a diaphragm; applying a reference pressure to a rear side of the diaphragm, wherein the diaphragm comprises a semiconductor Wheatstone bridge configured to provide an output indicative of a difference between the main and reference pressures; placing a coiled tube between one of the front or a rear diaphragm surfaces and one of the main or reference pressure sources having the sinusoidally varying pressure fluctuation, respectively, wherein the coiled tube is dimensioned to suppress the fluctuation.
 9. The method according to claim 8, wherein the sinusoidally varying pressure fluctuation is pump ripple produced by a pump where pressure is monitored as the reference pressure.
 10. The method according to claim 9, wherein the coiled tube is dimensioned according to the following equation: F _(n)=√(3πr ² c ²/4LV)/2π Where F_(n)=frequency of the pump ripple r=radius of tube c=velocity of sound in the pressurized monitored fluid L=length of coiled tube V=volume of cavity.
 11. The method according to claim 9, wherein the pump ripple frequency is between 3000 Hz to 5000 Hz.
 12. The method according to claim 9, wherein the semiconductor Wheatstone bridge comprises piezoresistors.
 13. A differential pressure transducer for providing an output proportional to a difference between a main pressure P₁ and a reference pressure P₂, the differential pressure transducer comprising: a housing comprising an internal hollow; a pressure sensor positioned in the housing, the pressure sensor comprising a deflectable diaphragm, wherein the deflectable diaphragm comprises a top surface and a bottom surface, wherein a pressure sensitive element is positioned on the deflectable diaphragm, wherein the pressure sensor provides an output according to a magnitude of deflection of the deflectable diaphragm; a first port in a surface of the housing for receiving the main pressure P₁; a first channel directed from the first port to communicate with the top surface of the deflectable diaphragm; a second port in the surface of the housing for receiving the reference pressure P₂; a second channel directed from the second port into the internal hollow; a tube coupled to the second channel and having a coiled tubular section dimensioned to suppress a ripple caused by operation of a pump, the tube comprising an end communicating with the bottom surface of the deflectable diaphragm to cause the pressure sensor to produce an output proportional to P₁−P₂.
 14. The differential pressure transducer according to claim 13, wherein the sensor is a semiconductor die having an active diaphragm area with piezoresistors located on the active diaphragm area and arranged in a Wheatstone bridge configuration.
 15. The differential pressure transducer according to claim 13, wherein the pump is a gear pump.
 16. The differential pressure transducer according to claim 13, wherein the second port is modeled as a series of pipes representing the second port, the second channel, the sensor having a cavity in front of the pressure transducer and where the resonant frequency Fn of the pipe/cavity system is given by: F _(n)=√(3πr ² c ²/4LV)/2π Where r=internal radius of pipe C=velocity of sound in the pressure fluid L=length of pipe V=volume of the cavity.
 17. The differential pressure transducer according to claim 16, wherein the coiled tubular section is dimensioned according to the formula for Fn.
 18. The differential pressure transducer according to claim 13, wherein the coiled tubular section is wound on a mandrel.
 19. The differential pressure transducer according to claim 13, wherein the pump ripple frequency is between 3000 Hz and 5000 Hz. 